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Bird Eye 400

Posted on September 21, 2026 By

The Bird Eye 400 is a typical representative of the light aircraft class, weighing approximately 5 kg, designed for reconnaissance and surveillance at lower altitudes. It operates within a 10-40 km radius from the ground control station, providing real-time intelligence data. Its primary task is to supply units with information about the situation “beyond the nearest hill (or house).”.

Table of Contents

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    • Overview and Operational Role
    • Technical Specifications and Performance
    • Integrated System and Payload
    • Technical Specifications
  • Image and diagram gallery of the Bird Eye 400
    • How to cite this article:

Overview and Operational Role

This Israeli apparatus is a classic light, man-portable reconnaissance UAV, intended for operations at the squad-platoon level. The entire complex fits into just two backpacks carried by infantrymen, making it effectively usable by special forces groups as well. It is a highly mobile and adaptable system for various missions.

Technical Specifications and Performance

The Bird Eye 400 is a compact aircraft, with a length of just 0.8 m and a wingspan of 2.2 m. It has a maximum takeoff weight of 5.6 kg and can carry a payload of 1.2 kg. A miniature electric motor provides the Bird Eye 400 with a flight duration of about one hour, a maximum operational radius of 10 km, and a flight altitude of about 3400 m.

Integrated System and Payload

Despite its small payload capacity, the UAV carries a very effective “Micro POP” observation and reconnaissance system. This system is built on an open architecture principle, allowing rapid replacement of sensor blocks, choosing between a day TV camera or an IR camera as needed. It is also equipped with communication and data exchange equipment for line-of-sight operation.

The complete “two-backpack” complex requires a two-person combat crew for operation. It includes three UAVs, a set of target opto-electronic equipment, a portable control panel, a communication complex, power sources, and a repair kit, ensuring self-sufficient operation in the field.

Technical Specifications

Modification Bird Eye 400
Wingspan, m 2. 20
Length, m 0. 80
Payload 1.20
Maximum takeoff weight 5.60
Engine type 1 Electric motor
Power, hp 1 х
Maximum speed, km/h 83
Range, km 10
Flight endurance, h 1
Service ceiling 3400

Image and diagram gallery of the Bird Eye 400

Bird Eye 400. Photography: IAI
Bird Eye 400. Photography: IAI
Bird Eye 400. Photography: IAI
Bird Eye 400. Photography: IAI
Bird Eye 400. Photography: IAI
Bird Eye 400. Photography: IAI
Bird Eye 400. Photography: IAI
Bird Eye 400. Photography: IAI
Bird Eye 400. Photography: Vitaly Kuzmin
Bird Eye 400. Photography: Vitaly Kuzmin

How to cite this article:

APA: Bird Eye 400 (). Bird Eye 400. wp.archivoaereo.com. https://wp.archivoaereo.com/en/bird-eye-400-2/
VANCOUVER: Bird Eye 400 [online]. wp.archivoaereo.com; [cited 2026-09-21]. Available at: https://wp.archivoaereo.com/en/bird-eye-400-2/
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